A Unified Nonlinear Adaptive Approach for Detection and Isolation of Engine Sensor, Actuator and Component Faults

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$599,479.00
Award Year:
2010
Program:
SBIR
Phase:
Phase II
Contract:
NNX10CA29C
Award Id:
90571
Agency Tracking Number:
084420
Solicitation Year:
n/a
Solicitation Topic Code:
A1
Solicitation Number:
n/a
Small Business Information
200 Canal View Blvd., Rochester, NY, 14623
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
073955507
Principal Investigator:
Liang Tang
Principal Investigator
(585) 424-1990
liang.tang@impact-tek.com
Business Contact:
Carol Marquardt
Business Official
(585) 585-1923
carol.marquardt@impact-tek.com
Research Institution:
n/a
Abstract
Impact Technologies in collaboration with Pratt & Whitney and Wright State University, proposes to continue the development of an innovative nonlinear adaptive method for detecting and isolating sensor faults, actuator faults, and component faults for jet engines. In sharp contrast to many conventional methods which deal with either sensor faults or component faults but not both, our method considers all three types of faults under one unified framework. In the successful Phase I program, we have demonstrated the effectiveness of the approach via a proof-of-concept demonstration using NASA's C-MAPSS model. The objective of Phase II is to raise the TRL by comprehensive development/improvement of the prototype system, extensive performance evaluation, and close collaboration with Pratt & Whitney for technology transition. The success of this program will bring significant benefits to the propulsion industry by providing a cutting-edge engine diagnostics system with features that have never been available, including adaptive nonlinear engine model, adaptive threshold, transferrable-belief-model-based residual evaluation within a unified framework. These novel technologies will greatly improve performance of onboard engine diagnostics system especially during transient operations and further reduce false alarm rate and missed detection rate, resulting in improved flight safety and significant reduction in overall engine maintenance cost.

* information listed above is at the time of submission.

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